Evaluation of impact-induced damages of composite structures using memory effects of metal-coated optical fiber sensors금속 코팅된 광섬유 센서의 기억 효과를 이용한 복합재 구조물의 충격 손상 평가

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In this study, a damage evaluation concept using the memory effect of metal-coated optical fiber sensors (MCOFSs) was proposed to evaluate impact-induced damages of composite structures. Two kinds of MCOFSs, i.e., aluminum-coated (Al-coated) FBG sensors and tin-coated FBG sensors, were fabricated. For Al-coated FBG sensors, a finite element analysis (FEA) was performed to investigate the capability of producing residual strain. For tin-coated FBG sensors, the capability of producing residual strain as well as the tensile failure strength was examined by experiments. It was confirmed that the induced quantity of the residual strain by MCOFSs increased with an increase of the applied strain. Then, a theoretical model for surface bonded MCOFSs on host structures was proposed. The distributions of the permanently induced residual strain in the core of the MCOFS were calculated by analytical and numerical methods when external loads were applied to the host and subsequently removed. The results were verified by laboratory experiments using the Al-coated FBG sensors bonded on carbon fiber reinforced polymer (CFRP) composite specimens. The memory effect of the MCOFS was confirmed by presenting the relationship between the residual strains of the Al-coated FBG sensors and the maximum strains experienced by the composite specimens. The effects of the material and geometric parameters of adhesive layers on the strain transfer coefficient, the residual strains, and the sensitivity coefficient of MCOFSs were investigated by a FEA, and the results were verified by laboratory experiments using the Al-coated FBG sensors. It was found that using a very soft adhesive with high non-linearity and plasticity should be avoided when` building MCOFS systems in actual situations. Moreover, small underlying adhesive thickness as well as short bonding length is favorable to achieve better performances. A response surface model among the system parameters was proposed based on the F...
Advisors
Lee, Inresearcher이인
Description
한국과학기술원 : 항공우주공학전공,
Publisher
한국과학기술원
Issue Date
2014
Identifier
568634/325007  / 020115039
Language
eng
Description

학위논문(박사) - 한국과학기술원 : 항공우주공학전공, 2014.2, [ viii, 148 p. ]

Keywords

FBG sensors; 충격 해석; 충격 실험; 원통형 복합재 구조물; 복합재 평판; 잔류 변형률; Residual strains; Composite plates; Composite cylinder; Impact tests; Impact analysis; FBG 센서

URI
http://hdl.handle.net/10203/196172
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=568634&flag=dissertation
Appears in Collection
AE-Theses_Ph.D.(박사논문)
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